Response of Simple Turbulence Models to Step Changes of Slip Velocity
Author:
Affiliation:
1. Federal Scientific Center “Applied Chemistry”, 197198, St. Petersburg, Russia
2. The Boeing Company, Seattle, Washington 98124-2207
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1301
Reference11 articles.
1. A low‐shear turbulent boundary layer
2. Experimental study of a three-dimensional, shear-driven, turbulent boundary layer
3. Experiments on the behaviour of an axisymmetric turbulent boundary layer with a sudden circumferential strain
4. Behavior of a Turbulent Boundary Layer Subjected to Sudden Transverse Strain
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